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Aeronautical Research Council Current Papers: Recent submissions
Now showing items 161-180 of 1393
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Measurement of the internal performance of a rectangular air intake mounted on a fuselage at mach numbers from 1.6 to 2 part 4
C. S. Brown
;
E. L. Goldsmith
(
1974
)
A prediction method for pressure distributions on compression surfaces of conical bodies at supersonic speeds
M. J. Larcombe
(
1974
)
Non-linear stability theory of the flat plate boundary layer
D. Corner
;
M. D. J. Barry
;
M. A. S. Ross
(
1974
)
Low-speed wind-tunnel tests on the lift-dependent drag of delta wings with conical camber
D. L. I. Kirkpatrick
;
P. J. Butterworth
(
1974
)
A shock capturing method for calculating supersonic flow fields
F. Walkden
;
P. Caine
(
1974
)
Some predictions of crack propagation under combined cabin pressurisation and acoustic loadings
W. T. Kirkby
(
1974
)
Study of solid state remote control techniques as applied to the redesign of the electrical system in a large civil aircraft
L. V. C. Jones
(
1974
)
An aeroelastic model helicopter rotor
R. Cansdale
(
1974
)
A two-dimensional aerofoil oscillating at low frequencies in high subsonic flow
D. Nixon
(
1974
)
Civil aircraft airworthiness data recording programme uneven runways encountered by subsonic jet transport aircraft during scheduled airline operations
G. B. Hutton
(
1974
)
Free-stream turbulence effects on the turbulent boundary layer
R. L. Evans
(
1974
)
Application of a variational method in plane compressible flow calculation
H. Rasmussen
;
N. Heys
(
1974
)
Comparison between dynamic stability boundaries for NPL 9615 and NACA 0012 aerofoils pitching about the quarter-chord
A. W. Moore
;
N. C. Lambourne
;
L. Woodgate
(
1974
)
High subsonic flow past a steady two-dimensional aerofoil
D. Nixon
;
G. J. Hancock
(
1974
)
Gust loads on 707 and VC 10 aircraft
I. W. Kaynes
(
1974
)
Human engineering studies of high speed pedestrian conveyors
A. C. Browning
(
1974
)
Results of a series of wind tunnel tests on the victor B.Mk.2 aircraft and a comparison with drag estimates and full scale flight data
J. I. Simper
(
1974
)
Development of a model technique for investigating the performance of soft-ground arresters for aircraft
J. R. Barnes
(
1974
)
Fatigue tests on plain specimens of titanium 6A1-4V under variable amplitude loading
A. W. Cardrick
;
B. H. E. Perrett
(
1974
)
The development of rapid-testing techniques for flutter experiments
K. W. Newman
;
C. W. Skingle
;
D. R. Gaukroger
(
1974
)
Now showing items 161-180 of 1393
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